JPS5886405U - Radial turbine nozzle support structure - Google Patents

Radial turbine nozzle support structure

Info

Publication number
JPS5886405U
JPS5886405U JP18214181U JP18214181U JPS5886405U JP S5886405 U JPS5886405 U JP S5886405U JP 18214181 U JP18214181 U JP 18214181U JP 18214181 U JP18214181 U JP 18214181U JP S5886405 U JPS5886405 U JP S5886405U
Authority
JP
Japan
Prior art keywords
nozzle
support structure
flange
radial turbine
attached
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
JP18214181U
Other languages
Japanese (ja)
Inventor
牛島 雄二
Original Assignee
日産自動車株式会社
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by 日産自動車株式会社 filed Critical 日産自動車株式会社
Priority to JP18214181U priority Critical patent/JPS5886405U/en
Publication of JPS5886405U publication Critical patent/JPS5886405U/en
Pending legal-status Critical Current

Links

Abstract

(57)【要約】本公報は電子出願前の出願データであるた
め要約のデータは記録されません。
(57) [Summary] This bulletin contains application data before electronic filing, so abstract data is not recorded.

Description

【図面の簡単な説明】[Brief explanation of the drawing]

第1図は従来め)シアルタービンノズルの支持構造の一
例を上半部のみ示す断面図、第2図は本考案ラジアルタ
ービンノズルの支持構造の一例を上半部のみ示す断面図
、第3図はそのタービンノズルを詳細に示す斜視図、第
4図はその支持ピンの形状を示す斜視図、第5図は本考
案の他の実施例を示す断面図、第6図AおよびBはその
支持ピンおよび板ばねの形状の一例を示すそれぞれ斜視
図である。 1・・・・・・ノズル翼、IA・・・・・・ノズル部、
2・・・・・・タービンロータ、3・・・・・・フラン
ジ部、4・・・・・・ホルダ、5・・・・・・スクロ=
ル、5A・・・・・・フランジ部、6−−−−−−ピン
、7・・・・・・ワッシャ、8・・・・・・ナツト、9
・・・・・・コイルばね、10・・・・・・タービンシ
ュラウド、11・・・・・・ベアリングハウジング、1
2・・・・・・軸受、13・・・・・・タービン軸、1
4. 15−−−−−−シールリング、21・・・・・
・ノズル翼、21A・・・・・・タービンノズル、22
・・・・・・フランジ、22A・・・・・・内周面、2
3・・・・・・切欠き溝、24・・・・・・段付き部、
i5・・・・・・支持ピン、25A・・・・・・頭部、
25B・・・・・・ばね止め部、26・・・・・・フラ
ンジ、27・・・・・・ベアリングハウジング(ノズル
取付部材)、27A・・・・・・内周面、28・・・・
・・ベアリングハウジング、29・・・・・・切欠き溝
、30・・・・・・ばね、31・・・・・・嵌め込み溝
、31A・・・・・・壁部、35・・・・・・ピン、3
5A・・・・・・頭部、35B・・・・・・軸部、35
C・・・・・・ばね止め部、36・・・・・・ばね。
Fig. 1 is a sectional view showing only the upper half of an example of the support structure of a conventional radial turbine nozzle, Fig. 2 is a sectional view showing only the upper half of an example of the support structure of the radial turbine nozzle of the present invention, and Fig. 3 is a perspective view showing details of the turbine nozzle, FIG. 4 is a perspective view showing the shape of its support pin, FIG. 5 is a sectional view showing another embodiment of the present invention, and FIGS. 6A and B are its support. FIG. 3 is a perspective view showing an example of the shapes of a pin and a leaf spring, respectively. 1... Nozzle blade, IA... Nozzle part,
2...Turbine rotor, 3...Flange part, 4...Holder, 5...Scroll=
5A...Flange part, 6------Pin, 7...Washer, 8...Nut, 9
......Coil spring, 10...Turbine shroud, 11...Bearing housing, 1
2...Bearing, 13...Turbine shaft, 1
4. 15---Seal ring, 21...
・Nozzle blade, 21A...Turbine nozzle, 22
...Flange, 22A ...Inner peripheral surface, 2
3...Notch groove, 24...Stepped part,
i5...Support pin, 25A...Head,
25B... Spring stopper, 26... Flange, 27... Bearing housing (nozzle mounting member), 27A... Inner peripheral surface, 28...・
... Bearing housing, 29 ... Notch groove, 30 ... Spring, 31 ... Fitting groove, 31A ... Wall part, 35 ... ...Pin, 3
5A...Head, 35B...Shaft, 35
C...Spring stop part, 36...Spring.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] ノズル翼および該ノズル翼が取付けられてタービンシュ
ラウドとの間にタービンロータへ4の高温ガス通路を形
成するフランジを有し、ノズル取付部材に取付けられた
ラジアルタービンノズルの支持構造において、前記フラ
ンジに係止溝を形成し、該係止溝に一端を係止させたピ
ンを、当該ピンの他端と前記ノズル取付部材との間に介
装した弾性部材により該ノズル取付部材側に付勢し°C
1前記フランジを前記ノズル取付部材に取付けたことを
特徴とするラジアルタービンノズルの支持構造。
In a support structure for a radial turbine nozzle attached to a nozzle mounting member, the support structure includes a nozzle vane and a flange to which the nozzle vane is attached to form four high-temperature gas passages to the turbine rotor between the nozzle vane and a turbine shroud, and the flange is attached to the flange. A locking groove is formed, and a pin having one end locked in the locking groove is urged toward the nozzle mounting member by an elastic member interposed between the other end of the pin and the nozzle mounting member. °C
1. A support structure for a radial turbine nozzle, characterized in that the flange is attached to the nozzle attachment member.
JP18214181U 1981-12-09 1981-12-09 Radial turbine nozzle support structure Pending JPS5886405U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP18214181U JPS5886405U (en) 1981-12-09 1981-12-09 Radial turbine nozzle support structure

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP18214181U JPS5886405U (en) 1981-12-09 1981-12-09 Radial turbine nozzle support structure

Publications (1)

Publication Number Publication Date
JPS5886405U true JPS5886405U (en) 1983-06-11

Family

ID=29980243

Family Applications (1)

Application Number Title Priority Date Filing Date
JP18214181U Pending JPS5886405U (en) 1981-12-09 1981-12-09 Radial turbine nozzle support structure

Country Status (1)

Country Link
JP (1) JPS5886405U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2014037828A (en) * 2012-08-14 2014-02-27 General Electric Co <Ge> Turbine aperture cap system

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2014037828A (en) * 2012-08-14 2014-02-27 General Electric Co <Ge> Turbine aperture cap system

Similar Documents

Publication Publication Date Title
JPS60175914U (en) oil bearing
JPS5886405U (en) Radial turbine nozzle support structure
JPS59175607U (en) Seal ring for axial flow fluid machinery
JPS5973503U (en) Ceramic bottle housing
JPS63183432U (en)
JPS5941602U (en) Support device for ceramic parts
JPS60178388U (en) Pump shaft support structure
JPS60195934U (en) Turbocharger heat insulator
JPS58163301U (en) Resin hub ornament
JPS6098702U (en) turbine moving blade
JPS5932103U (en) Radial turbine nozzle support device
JPS6039703U (en) Turbine missile prevention device
JPS5965906U (en) Ceramic container structural members
JPS59141102U (en) Gas turbine stator blade shroud structure
JPS6125503U (en) Gas turbine with ceramic rotor blades
JPS58142302U (en) axial flow turbomachinery
JPS591927U (en) Floating bearing for turbocharger
JPS604789U (en) Vanes of rotary compressors, etc.
JPS58104301U (en) Ceramic radial turbine rotor
JPS6117402U (en) gas turbine engine
JPS59192700U (en) Blower
JPS6097301U (en) Variable nozzle radial turbine
JPS5927705U (en) hair dryer
JPS60152003U (en) Turbine rotor assembly
JPS59165987U (en) Roots pump rotor support structure